AU2009248619B2 - Steel with high properties for solid parts. - Google Patents
Steel with high properties for solid parts. Download PDFInfo
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- AU2009248619B2 AU2009248619B2 AU2009248619A AU2009248619A AU2009248619B2 AU 2009248619 B2 AU2009248619 B2 AU 2009248619B2 AU 2009248619 A AU2009248619 A AU 2009248619A AU 2009248619 A AU2009248619 A AU 2009248619A AU 2009248619 B2 AU2009248619 B2 AU 2009248619B2
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 60
- 239000010959 steel Substances 0.000 title claims abstract description 60
- 239000007787 solid Substances 0.000 title description 2
- 239000000203 mixture Substances 0.000 claims abstract description 21
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 14
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 10
- 239000000126 substance Substances 0.000 claims abstract description 9
- 229910052717 sulfur Inorganic materials 0.000 claims abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 6
- 229910052802 copper Inorganic materials 0.000 claims abstract description 6
- 239000012535 impurity Substances 0.000 claims abstract description 6
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- 238000004519 manufacturing process Methods 0.000 claims description 20
- 210000003462 vein Anatomy 0.000 claims description 19
- 238000001816 cooling Methods 0.000 claims description 16
- 238000010791 quenching Methods 0.000 claims description 12
- 230000000171 quenching effect Effects 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 11
- 239000004033 plastic Substances 0.000 claims description 9
- 229920003023 plastic Polymers 0.000 claims description 9
- 238000005242 forging Methods 0.000 claims description 7
- 238000005096 rolling process Methods 0.000 claims description 7
- 238000007493 shaping process Methods 0.000 claims description 7
- 229910000734 martensite Inorganic materials 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 abstract description 8
- 238000003723 Smelting Methods 0.000 abstract 1
- 235000019589 hardness Nutrition 0.000 description 40
- 230000000694 effects Effects 0.000 description 18
- 238000005204 segregation Methods 0.000 description 18
- 229910052799 carbon Inorganic materials 0.000 description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 16
- 239000011651 chromium Substances 0.000 description 12
- 239000011572 manganese Substances 0.000 description 12
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- 238000005496 tempering Methods 0.000 description 12
- 238000005275 alloying Methods 0.000 description 11
- 238000011282 treatment Methods 0.000 description 10
- 238000010438 heat treatment Methods 0.000 description 8
- 230000002349 favourable effect Effects 0.000 description 7
- 239000011733 molybdenum Substances 0.000 description 7
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 6
- 230000008901 benefit Effects 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 6
- 239000011669 selenium Substances 0.000 description 6
- 239000010703 silicon Substances 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011593 sulfur Substances 0.000 description 5
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- 229910052720 vanadium Inorganic materials 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 239000010955 niobium Substances 0.000 description 3
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 3
- 239000000047 product Substances 0.000 description 3
- 229910052711 selenium Inorganic materials 0.000 description 3
- 229910052714 tellurium Inorganic materials 0.000 description 3
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 229910017083 AlN Inorganic materials 0.000 description 1
- PIGFYZPCRLYGLF-UHFFFAOYSA-N Aluminum nitride Chemical compound [Al]#N PIGFYZPCRLYGLF-UHFFFAOYSA-N 0.000 description 1
- ZAKOWWREFLAJOT-CEFNRUSXSA-N D-alpha-tocopherylacetate Chemical compound CC(=O)OC1=C(C)C(C)=C2O[C@@](CCC[C@H](C)CCC[C@H](C)CCCC(C)C)(C)CCC2=C1C ZAKOWWREFLAJOT-CEFNRUSXSA-N 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 230000002040 relaxant effect Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 230000011218 segmentation Effects 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 150000004763 sulfides Chemical class 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0242—Flattening; Dressing; Flexing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0081—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for slabs; for billets
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Articles (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Abstract
High-strength steel, the chemical composition of which comprises, by weight: 0.03% ≤ C < 0.2%, Si ≤ 0.49%, 3% < Mn ≤ 4%, Ni ≤ 0.9%, 1% ≤ Cr ≤ 5%, Mo + W/2 ≤ 1%, Cu ≤ 0.9%, S +Se/2 + Te/3 < 0.020% and Al ≤ 0.1%, the rest being iron and impurities resulting from the smelting. Block and sheets obtained.
Description
High-characteristic steel for large-size parts The present invention relates to a high-strength steel intended, in particular, for the manufacture of large-size parts such as parts of moulds for plastics materials, tooling parts such as dies, or wear parts such as abrasion-resistant parts. For numerous applications, the mechanical parts which are subjected to high stresses or to very high wearing loads have to be produced from steels having high mechanical strengths corresponding to hardnesses of between 300 and 500 HB, but which must nevertheless remain sufficiently tough, machinable, weldable, etc. These parts are generally obtained by cutting and machining plates or blocks of great thickness. A block having a generally parallelepipedal shape is obtained by forging an ingot. A plate is obtained by rolling an ingot or a slab. For these articles of generally parallelepipedal shape, the thickness is the smallest dimension. For the blocks or plates in question here the thickness is greater than 10 mm and can be as great as 1 metre. The existence of hard points is often observed on blocks or plates of this type consisting of the aforementioned steels, owing to segregation. This segregation corresponds to local variations in chemical composition resulting from solidification phenomena of the ingots from which the blocks are produced. These hard points have several drawbacks. They may have the effect of making uniform machining or polishing difficult, and this may pose problems in the production of 2 parts for which geometric precision and surface quality are important. These variations in hardness may also have the effect of creating brittle regions which may be preferential sites for the initiation of cracks that are detrimental, in particular, to the overall toughness of the parts, but also to the weldability or suitability for thermal cutting of the parts. The greater the section of the parts in question, the more pronounced these segregation problems are. This is the case, in particular, with parts having sections which may be as much as several decimetres or even more than 1 metre, in particular owing to the need to add a large quantity of alloying elements in order to obtain sufficient quenchability to permit the production of such parts. To reduce the size of these segregated regions, ingot manufacturing methods of the electroslag remelting (ESR) or vacuum remelting type are sometimes employed. These methods are particularly effective for obtaining very homogeneous large-size parts which consequently have satisfactory properties in service. However, they have the drawback of being extremely expensive. Therefore, these methods are basically used for very high performance parts which, in view of their uses, can justify very high manufacturing costs. To reduce the effect of this segregation, the use of homogenizing heat treatments has also been proposed. The object of these heat treatments is to reduce the local variations in chemical composition by diffusing the chemical elements from the regions with the highest content to the regions with the lowest content. They have the drawback of 3 being extremely lengthy and therefore of being extremely expensive. It is an object of the present invention to overcome at least one of these drawbacks by providing a steel for obtaining high mechanical characteristics which may be as high as 5 400 HB, or even 450 HB, even in the core of very bulky parts, while having relatively slight variations in hardness due to segregation. In a first aspect, the present invention provides a steel block or plate having a thickness greater than or equal to 20 mm and a composition comprising by weight: 10 0.03% 5 C < 0.2% Si < 0.49% 3% < Mn < 4% Ni S 0.9% 15 1% < Cr < 5% Mo+W/2 < 1% Cu 5 0.9% S +Se/2+ Te/3 < 0.020% Al 5 0.1%, 20 the remainder being iron and impurities resulting from production, wherein the steel has a bainitic, martensito-bainitic or martensitic structure, and in that the difference in hardness between the harder regions and the less hard regions of the block or plate, resulting from the segregated veins, is less than 20% of the average hardness of the block. 25 In a second aspect, the present invention provides a method for manufacturing a steel block or plate according to the first aspect, wherein, after shaping by hot plastic deformation by forging or rolling, quenching is carried out by air cooling. 30 In a third aspect, the present invention provides a method for manufacturing a steel block or plate according to the first aspect, wherein, after shaping by hot plastic deformation by forging or rolling, austenitization is carried out and is followed by quenching by air cooling.
3a In a fourth aspect, the present invention provides a steel block or plate produced by the method of the second aspect. In a fifth aspect, the present invention provides a steel block or plate produced by the 5 method of the third aspect. The invention also relates to a high-strength steel of which the chemical composition comprises, by weight: 1o 0.03% 5 C < 0.2% Si 5 0.49% 3% < Mn < 4% Ni < 0.9% 1% 5 Cr S 5% is Mo+W/2 < 1% Cu 5 0.9% S +Se/2 + Te/3 < 0.020% Al < 0.1%, 20 the remainder being iron and impurities resulting from production. Preferably, the chemical composition satisfies one or more of the following conditions: Cr > 2.5% 25 Cr < 3.5% Ni < 0.5% Cu < 0.4% 4 Mo + W/2 0.3%. In particular, in a preferred embodiment, the chemical composition is such that: 2.7% Cr 3% Mo 0.3%. The invention also relates to a steel block or plate according to the invention having a thickness greater than 20 mm and a bainitic, martensito-bainitic or martensitic structure and of which the difference in hardness between the harder regions and the less hard regions of the block or plate, resulting from the segregated veins, is less than approximately 20% of the average hardness of the block. The invention finally relates to a method for manufacturing a steel block or plate according to the invention whereby, after shaping by hot plastic deformation by forging or rolling, quenching is carried out by air cooling or austenitization is carried out and is followed by quenching by air cooling. The invention is particularly suitable for the manufacture of plates or blocks having a thickness greater than 20 mm. This thickness can exceed 100 mm and even exceed 150 mm, even 300 mm, and even 500 mm. It may be as great as 1 metre. The invention will now be described in a more detailed, but non-limiting, manner with reference to the single appended Figure and will be illustrated by examples.
5 The appended Figure is a graph showing the desired carbon content as a function of the desired hardness of a high characteristic steel according to the invention, after tempering at 5500C (line 1) or after tempering below 5000C (line 2), for a basic composition: 0.15% of silicon, 3.3% of manganese, 3% of chromium, 0.25% of molybdenum and for blocks which have been air-cooled after normalizing at 9000C. In order to produce parts having very great thicknesses, the thickness being greater than 20 mm and possibly being as great as 500 mm or even exceeding 1 metre, and in order that the average hardness is extremely homogeneous between the core and the surface, it is necessary to use a steel of which the quenchability is sufficient to obtain a homogeneous structure without the need to carry out quenching in an excessively harsh quenching medium. The harsher the quenching medium, the greater the variations in the cooling rates within the block and therefore the greater the risks of obtaining a heterogeneous structure. However, when quenchability is adequate air cooling and, in particular, still air cooling, which leads to relatively modest differences in cooling between the surface and the core leads to a satisfactory structure which is therefore extremely homogeneous. These quenching conditions obviously do not have a direct influence on the problem of local variations in hardness resulting from segregation. In order to achieve adequate quenchability, it is generally considered necessary to use chemical compositions having a high content of alloying elements. However, these alloying elements have the effect of inducing segregation which may be significant.
6 Although it is generally considered that the greater the tendency of the alloying elements to segregate, the greater their influence on the difference in hardness of the segregated veins is, the inventors have found, in a completely novel and unexpected manner, that there was no correlation between the intensity of the overhardening into the segregated vein in alloying elements and the respective propensities of each of these alloying elements to segregate. The propensity of the alloying elements to segregate and their effects on the hardnesses of the segregated veins is illustrated by the following tests, during which steel was cast in six batches into ingots of 3 tonnes having the compositions, expressed as 10~3% by weight, shown in Table 1. Table 1 C Si Mn Cr Mo Ni 1 170 200 1500 2800 100 1500 2 170 500 1500 2800 100 1500 3 170 200 2800 2800 100 1500 4 170 200 1500 1300 100 1500 5 170 200 1500 2800 400 1500 6 170 200 1500 2800 100 200 These ingots were rolled into 50 mm thick plates which were cut up into samples of which both the average hardness and the hardenings due to segregation were measured. The samples taken from each of the plates were examined on the one hand in the as-cooled state in which they had a martensitic structure and on the other hand in the state in which they had been tempered at a temperature of 500 0 C at which they had a tempered martensitic structure.
7 The following was measured concurrently in the segregated veins of each of the samples: - the average degrees of segregation of each of the different alloys (Si, Mn, Cr, Mo, Ni), by means of microprobe determination. The tendency to segregate inherent in each element was characterized by means of the ratio (%) relating to the difference between average segregated vein composition Cv and composition during casting CO to the value of the latter (namely: (Cv - CO)/CO); - the average hardness of the segregated veins, by means of conventional Vickers type tests under 300 g. The overhardening into veins corresponds to the difference between the average hardness of the veins and that of the surrounding matrix outside the veins. By subsequently comparing these measurements between pairs of castings it is possible to deduce the contribution to the overhardening into veins attributable specifically to the segregation of each alloying element. The proportion of overhardening into veins attributable to an element is the resultant of the segregation of this element, in other words, by definition, the product of the nominal content of this element times its degree of segregation. Consequently, the elements will be validly compared with regard to their harmfulness in this regard by relating in each case the contribution to the overhardening to the same reference level of nominal content (0.2% was selected arbitrarily). Thus, by way of example, the difference in average hardness of 33 HV found between castings 1 and 3 (with 1.5% and 2.8% of 8 Mn) leads to evaluation of an overhardening of 33x(O.2% / 1.3%) = 5 Hv for 0.2% of Mn (cf. table below). The results are shown in Table 2 below. Table 2 Alloying Inherent tendency of Overhardening effect (Hv) found in elements the element to segregate segregated veins related to 0.2 % of alloy (after tempering) Si 35% 8 Cr 26% 17 Mn 42% 5 Mo 67% 70 Ni 32% 3 Expressed in qualitative terms, the inherent tendency of each element to segregate and its effect of hardening into segregated vein are set out in Table 3 below. Table 3 Alloying element Inherent tendency of the Overhardening effects (Hv) element to segregate found in segregated veins Si Medium Slight Cr Slight Medium Mn Fairly strong Very slight Mo, V Strong Very strong Ni Medium Very slight In view of these results, it appears that, contrary to generally accepted ideas, in order to achieve very good quenchability with slight segregation, it is desirable to select a composition comprising a large amount of manganese, little chromium and little molybdenum. It may also be beneficial to provide a large amount of nickel. As nickel is a very expensive element, however, it is preferable to use manganese rather than nickel.
9 These results show that, to produce steels for the manufacture of very large size parts having high characteristics and having relatively slight variations in hardness due to segregation, it is desirable to use a steel of which the composition satisfies the following conditions: - carbon: from 0.03% to 0.2% as a % by weight. This element has the main effect of acting on the hardness of the martensite, its content therefore being selected as a function of the degree of hardness desired in the parts. To determine the carbon content as a function of the desired hardness, the scale of hardness can for example be divided into tranches of 40 HB, between 320 HB and 440 HB. These ranges correspond approximately to conventional ranges of use of abrasion resistant steels or tooling steels. The following ranges of carbon content can also be considered: from 0.03% to 0.06% of carbon, from 0.07% to 0.15%, and from 0.16% to 0.20% of carbon. A range of hardness corresponds to each of these ranges of carbon content, for a given heat treatment. Depending on whether the steel has been tempered at about 550 0 C or has not been tempered or has only received a treatment at a temperature of substantially less than 5000C, the degree of hardness for an identical carbon content is not the same. In general, the lowest range of hardness corresponds to the lowest carbon content and the highest range of hardness to the highest carbon content. However, the boundaries of these ranges of carbon content corresponding to the hardnesses vary slightly as a function of the contents in the other alloying elements and as a function of the cooling rate and also as a function of the heat treatment carried out on the parts.
10 This segmentation is illustrated by an example of steel of which the composition comprises 0.15% of silicon, 3.3% of manganese, 3% of chromium and 0.25% of molybdenum in addition to the carbon. Fig. 1 shows the development of the hardness as a function of the carbon content for blocks which have been air cooled after normalizing to 900 0 C subsequent to prior hot rolling. The first block was tempered at 480 0 C and the second at 550 0 C. As shown in the drawing, the block which was tempered at the temperature of 480 0 C has a hardness of 360 HB with a carbon content of 0.1% whereas the same steel tempered at 5500C has a hardness of only 320 HB. Similarly, when the steel contains approximately 0.2% of carbon, the block tempered at 480 0 C has a hardness of approximately 440 HB whereas the block tempered at 5600C has a hardness of 375 HB. The minimum carbon content of 0.03% corresponds to a value below which the hardening segregation and the benefit attached to the reduction thereof become slight. It will be noted that the hardnesses obtained vary slightly by application of tempering once its temperature no longer exceeds substantially 480 0 C. These results are also applicable to plates. - silicon: This element which is used, in particular, to deoxidize the bath of liquid steel during production has a content which is generally greater than 0.025% and preferably greater than 0.05% or even possibly exceeds 0.1%. However, the content of this element must remain less than 0.49%, preferably less than 0.35% and more preferably less than 0.19% and, if possible in view of the deoxidation requirements of the bath, must remain less than 0.1%. Silicon is an element which tends to very significantly increase the large-scale segregation at the ingot head (known as major segregation), and this then has the effect of feeding the segregated veins which are therefore greater, the greater the segregation at the ingot head. In addition, the silicon tends to impair the thermal conductivity of the steel, and this may be unfavourable in some applications such as, in particular, moulds for the moulding of plastics material. Finally, silicon is detrimental to the sensitivity to brittleness of reversible tempering, which should be taken into consideration, in particular when the cooling rates of the products are low, which is the case in the applications in question for this steel. - chromium: This element has a favourable effect on the quenchability and, owing to its tendency to form carbides, has a favourable effect on the resistance to softening during tempering, and the effect of overhardening on the segregated veins is much less pronounced than that of molybdenum or tungsten. It must be added in contents which are preferably greater than 1% and more preferably greater than 2.5%, but which must remain less than 5% and preferably less than 3.5% and even more preferably be between 2.7% and 3% in order to obtain both adequate quenchability and satisfactory resistance to tempering softening, without leading to excessive overhardening of the segregated regions at the same time. - molybdenum and tungsten: These two elements, which have a very pronounced tendency to form carbides which promote high resistance to softening during tempering, do however have the drawback of having a very significant effect on the overhardening of the segregated regions. Therefore, as tungsten has the same effect as molybdenum in a proportion of 2% of tungsten per 1% of molybdenum, the sum Mo + W/2 will be limited to 1%, preferably 0.5% and even 0.3% maximum. - vanadium, niobium: As these elements have extremely undesirable effects on the overhardness of the segregated 12 regions, the steel will not receive voluntary additions of vanadium or niobium which could however exist in the state of residuals, the vanadium content having to remain less than 0.010% and preferably less than 0.005%, and the niobium content; having to remain less than 0.050% and preferably less than 0.010%. - manganese: This element has a very favourable effect on the quenchability and also has the advantage of having a very modest effect on the overhardness of the segregated regions. It is therefore preferably used for achieving quenchability. Therefore, the manganese content is between 3% and 4% so that the combined effect of the manganese and the carbon on the quenchability is adequate. - nickel: This element has a favourable effect on the quenchability and a modest effect on the overhardness of the segregated regions. However, this element is very expensive so its content is less than 0.9%, preferably less than 0.5% and even more preferably is merely at residual levels. - copper : The content of this element which is often present in the form of a residual must remain less than 0.9%, preferably less than 0.4% and more preferably even lower at less than 0.2%, since this element does not have a particularly favourable effect on the properties of the steel in question. - aluminium: This element which has a favourable effect on the, deoxidation of the liquid steel bath during production and, in the solid state, enables the austenitic grain size to be controlled by aluminium nitride formation has a content of less than 0.1%. When the sulfides possibly formed, which can form elongate networks which are the source of surface disintegration, are intended to be globulized, it is preferable to add from 0.040 to 0.60% of aluminium.
13 - sulfur, Se, Te: Sulfur, which is an impurity that is always present at least at trace levels, can have a favourable effect on machinability. If the contents are excessive, however, it has an unfavourable effect on the toughness and possibly on the polishability of the steels. Selenium and tellurium have effects comparable to that of sulfur in a proportion of 2 parts of selenium per 1 part of sulfur or of 3 parts of tellurium per 1 part of sulfur. Therefore, especially in applications requiring good polishability, the sum S + Se/2 + Te/3 is in the state of a trace level or greater than 0.005%, but remains less than 0.020% in any case. The remainder of the composition comprises iron and impurities resulting from production. To manufacture parts comprising the steel which has just been described, a steel with the selected composition is first produced, then this steel is cast in the form of a semi finished product, for example, an ingot, which is shaped by hot plastic deformation, either by forging or by rolling. The blank thus obtained, which forms a block of steel or a plate, is then used either in the as-rolled or as-forged state or after a heat treatment appropriate for the envisaged use selected by the person skilled in the art. The as-rolled or as-forged state is employed in particular for applications such as the manufacture of parts intended to resist wear in the mineral industry or civil engineering, in which applications the cost of the steel is a very important element of the selection.
14 When more specific properties are desired, the optionally cut or pre-machined as-forged or as-rolled parts, plates or blocks are austenitized by heating to a temperature greater than the temperature AC 3 , in general of about 9000C, and are then quenched by cooling in the open air, in particular in still air, or optionally in a quenching medium giving a slightly faster cooling, but without this being desired. This austenitization followed by air cooling has the advantage of enhancing the ratio of the elastic limit to the tensile strength. It will. be noted that the quenching treatment can, if necessary, be carried out directly in the heat of shaping by hot plastic deformation, if this has been carried out under appropriate temperature conditions. The person skilled in the art knows how to determine such conditions. The blocks or plates, whether in the hot-shaped state or reaustenitized and slowly cooled, can advantageously be subjected to a tempering heat treatment at a temperature greater than 450 0 C but of less than 5500C. A tempering treatment of this type, which does not significantly change the hardness, has the advantage of reducing the residual stress level in the tanks or the parts in the state as they leave the preceding treatments. This reduction in internal stresses is particularly advantageous for precision parts obtained after very significant machining by removal of material. From this point of view, the reaustenitization and slow cooling treatment has the advantage over the crude hot shaping state of relaxing at least some of the residual stresses.
15 Finally, the tempering treatment may have the advantage of further enhancing the ratio of the elastic limit to the tensile strength slightly. In a variation, the tempering treatment may be replaced by a stress--relieving treatment at a temperature of between 150 0 C and 2500C. A stress-relieving treatment of this type does not lead to appreciable variations in hardness. On the other hand, it generally leads to a significant improvement in toughness, and this is useful both for facilitating use of the products and for improving the service life of the parts. A treatment of this type is particularly appropriate for parts intended to work under conditions necessitating high resistance to wear due to metal-on-metal friction as encountered in mechanical engineering, or wear due to abrasion encountered in civil engineering, mines or quarries. By way of example, two castings of steel designated 1 and 2 were carried out and were compared with steels designated C1 and C2, given by way of comparison. With these steels having the compositions given in Table 4, 150 mr thick plates were manufactured by hot rolling and, after cooling, were reaustenitized by heating to 9000C, and were then air cooled.
16 Table 4 C Si Mn Ni Cr Mo V H dH dH/ Tf Weld Econ H(%) ability om C1 0.24 0.2 1.3 0.3 1.9 0.49 - 310 65 21 150 + ++ C2 0.53 0.4 0.8 1.6 1.1 0.55 0.11 395 119 30 41 + + Steel inv 1 0.11 0.10 3.4 0.2 2.9 0.28 - 340 41 12 135 +++ +++ tem 550*C Steel inv 2 0.13 0.15 3.2 0.2 3.0 0.22 - 405 48 15 105 ++ +++ tem 480*C The average Brinell hardness (H), the difference (dH) in hardness between the hardest portions of the segregated regions and the least hard portions of the plates, and the ratio between the hardness difference and the average density (dH/H in %), were measured on the plates obtained, the machinability was evaluated by a milling time (Tf) and the weldability and the economic value of the steel were also evaluated. The results which are also shown in Table 4 demonstrate that the steels according to the invention, while having hardnesses which may be relatively great as they range between 340 HB and 405 HB, have hardness variations which represent less than 15% of the average hardness as against more than 20% for steels according to the prior art. In addition, these steels have satisfactory machinability, are more suited to welding than the comparison steels and are more economical.
Claims (11)
1. Steel block or plate having a thickness greater than or equal to 20 mm and a composition comprising by weight: 5 0.03% 5 C < 0.2% Si < 0.49% 3% < Mn < 4% Ni S 0.9% 10 1% 5 Cr 5 5% Mo+W/2 < 1% Cu < 0.9% S +Se/2+ Te/3 < 0.020% Al < 0.1%, 15 the remainder being iron and impurities resulting from production, wherein the steel has a bainitic, martensito-bainitic or martensitic structure, and in that the difference in hardness between the harder regions and the less hard regions of the block or plate, resulting from the segregated veins, is less than 20% of the average hardness of the block. 20
2. Steel block or plate according to claim 1, wherein the chemical composition is such that: Cr > 2.5%. 25
3. Steel block or plate according to claim 1 or claim 2, wherein: Cr < 3.5%. 30
4. Steel block or plate according to any one of claims 1 to 3, wherein: Ni < 0.5%. 18
5. Steel block or plate according to any one of claims 1 to 4, wherein: Cu < 0.4%. s
6. Steel block or plate according to any one of claims I to 5, wherein: Mo + W/2 < 0.3%.
7. Steel block or plate according to any one of the preceding claims, wherein the io chemical composition is such that: 2.7% 5 Cr < 3% Mo 5 0.3%. 15
8. Method for manufacturing a steel block or plate according to any one of claims 1 to 7, wherein, after shaping by hot plastic deformation by forging or rolling, quenching is carried out by air cooling.
9. Method for manufacturing a steel block or plate according to any one of claims 1 20 to 7, wherein, after shaping by hot plastic deformation by forging or rolling, austenitization is carried out and is followed by quenching by air cooling.
10. A steel block or plate produced by the method of claim 8. 25
11. A steel block or plate produced by the method of claim 9. Dated 27 April, 2012 Industeel Creusot 30 Patent Attorneys for the Applicant/Nominated Person SPRUSON & FERGUSON
Applications Claiming Priority (3)
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| EP08300199.0 | 2008-05-06 | ||
| EP08300199A EP2123787A1 (en) | 2008-05-06 | 2008-05-06 | High-grade steel for massive parts. |
| PCT/FR2009/050822 WO2009141556A1 (en) | 2008-05-06 | 2009-05-05 | Steel with high properties for solid parts. |
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| AU2009248619A1 AU2009248619A1 (en) | 2009-11-26 |
| AU2009248619B2 true AU2009248619B2 (en) | 2012-05-24 |
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| US (2) | US9103008B2 (en) |
| EP (2) | EP2123787A1 (en) |
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| WO2016001699A1 (en) | 2014-07-03 | 2016-01-07 | Arcelormittal | Method for manufacturing a high strength steel sheet having improved formability and sheet obtained |
| WO2016001703A1 (en) | 2014-07-03 | 2016-01-07 | Arcelormittal | Method for manufacturing a high strength steel sheet and sheet obtained by the method |
| WO2016001705A1 (en) | 2014-07-03 | 2016-01-07 | Arcelormittal | Method for manufacturing a high strength steel sheet having improved formability and ductility and sheet obtained |
| EP3168312B1 (en) * | 2015-11-16 | 2019-04-10 | Deutsche Edelstahlwerke Specialty Steel GmbH & Co. KG | Engineering steel with bainitic structure, forged part produced therefrom and method for making a forged part |
| JP6493286B2 (en) * | 2016-04-19 | 2019-04-03 | Jfeスチール株式会社 | Abrasion resistant steel sheet and method for producing the abrasion resistant steel sheet |
| TWI756226B (en) * | 2016-06-30 | 2022-03-01 | 瑞典商伍德赫爾恩股份有限公司 | A steel for a tool holder |
| CN107287503A (en) * | 2017-06-07 | 2017-10-24 | 江苏科技大学 | One kind improves residual elements and deteriorates the thermoplastic method of steel |
| AU2019200375A1 (en) * | 2018-06-26 | 2020-01-16 | A. Finkl & Sons Co. | Plastic injection mold tooling and a method of manufacture thereof |
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| US5759299A (en) * | 1994-05-10 | 1998-06-02 | Nkk Corporation | Rail having excellent resistance to rolling fatigue damage and rail having excellent toughness and wear resistance and method of manufacturing the same |
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| JP2881869B2 (en) * | 1989-12-06 | 1999-04-12 | 大同特殊鋼株式会社 | Steel for plastic molds with excellent weldability |
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| FR2748036B1 (en) * | 1996-04-29 | 1998-05-22 | Creusot Loire | LOW ALLOYED STEEL FOR THE MANUFACTURE OF MOLDS FOR PLASTIC MATERIALS |
| FR2748037B1 (en) * | 1996-04-29 | 1998-05-22 | Creusot Loire | WELDABLE REPAIRABLE STEEL FOR THE MANUFACTURE OF MOLDS FOR PLASTIC MATERIALS |
| FR2764308B1 (en) * | 1997-06-04 | 1999-07-23 | Thyssen France Sa | PROCESS FOR THE MANUFACTURE OF A STEEL FOR LARGE DIMENSION MOLDS |
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| JP2001294973A (en) * | 2000-04-05 | 2001-10-26 | Daido Steel Co Ltd | Steel for plastic molds with excellent powder EDM |
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| FR2847271B1 (en) * | 2002-11-19 | 2004-12-24 | Usinor | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
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|---|---|---|---|---|
| DE651845C (en) * | 1935-10-20 | 1937-10-20 | Boehler & Co Akt Ges Geb | Steel alloy for hot work tools |
| JPH06184695A (en) * | 1992-12-22 | 1994-07-05 | Hitachi Ltd | Steel for metal mold for plastic molding excellent in weldability and machinability |
| US5759299A (en) * | 1994-05-10 | 1998-06-02 | Nkk Corporation | Rail having excellent resistance to rolling fatigue damage and rail having excellent toughness and wear resistance and method of manufacturing the same |
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| Publication number | Publication date |
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| EP2279275A1 (en) | 2011-02-02 |
| ZA201006646B (en) | 2011-06-29 |
| CA2718848A1 (en) | 2009-11-26 |
| TW201018735A (en) | 2010-05-16 |
| KR20120025009A (en) | 2012-03-14 |
| US20150299835A1 (en) | 2015-10-22 |
| CA2718848C (en) | 2013-02-12 |
| WO2009141556A1 (en) | 2009-11-26 |
| KR20110006671A (en) | 2011-01-20 |
| KR20140129385A (en) | 2014-11-06 |
| SI2279275T1 (en) | 2013-12-31 |
| BRPI0912251A2 (en) | 2015-10-06 |
| US20110108169A1 (en) | 2011-05-12 |
| UA95052C2 (en) | 2011-06-25 |
| PL2279275T3 (en) | 2014-03-31 |
| JP5001460B2 (en) | 2012-08-15 |
| AU2009248619A1 (en) | 2009-11-26 |
| RU2463373C2 (en) | 2012-10-10 |
| JP2011518957A (en) | 2011-06-30 |
| EP2123787A1 (en) | 2009-11-25 |
| TWI435938B (en) | 2014-05-01 |
| US9103008B2 (en) | 2015-08-11 |
| ES2435431T3 (en) | 2013-12-19 |
| CN102016097A (en) | 2011-04-13 |
| MX2010011495A (en) | 2010-11-12 |
| RU2010149330A (en) | 2012-06-20 |
| EP2279275B1 (en) | 2013-08-28 |
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